View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 20804U 90083A 23342.52150973 .00000063 00000-0 51090-4 0 9998
2 20804 82.9379 130.3253 0036121 328.7172 98.9454 13.74425185666629
| Epoch (UTC): | 08 December 2023 12:30:58 |
| Eccentricity: | 0.0036121 |
| inclination: | 82.9379° |
| perigee height: | 957 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 130.3253° |
| argument of perigee: | 328.7172° |
| revolutions per day: | 13.74425185 |
| mean anomaly at epoch: | 98.9454° |
| orbit number at epoch: | 66662 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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